Sliding Mode Control Deign for A Hypervelocity Flight Vehicle
Two sliding mode controllers are designed and analyzed for the longitudinal dynamics of a generic hypervelocity flight vehicle. This vehicle model is highly nonlinear and has to be linearized first. These two controllers are designed based on different sliding surfaces, one is basic form and the other is integral form. Simulation studies were conducted for trimmed cruise conditions of 110000 ft and Mach 15 where the responses of the vehicle to a step change in altitude and airspeed were evaluated.
Sliding Mode Control Hypervelocity Flight Vehicle Full State Feedback Linearization Tracking Control
Li Huifeng Li Zhaoying Zhao Wenhua
School of Aerospace Beijing University of Aeronautics and Astronautics,Beijing 100083 China
国际会议
The 11th International Space Conference of Pacific-basin Societies(第11届环太平洋国际航天会议)
北京
英文
322-327
2007-05-16（万方平台首次上网日期，不代表论文的发表时间）